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MSFS 2024 · Airliner
Fenix A320 (CEO) Emergency Procedures
Immediate Action Procedures
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7 procedures
- 1THR LEVERSIDLE
- 2After aircraft is stopped, PARK BRKON
- 3Affected ENG MASTEROFF
- 4Affected ENG FIRE pbPUSH
- 5AGENT 1 and 2DISCH
- 6Condition of affected engineASSESS
- 7If requiredACCOMPLISH EVACUATION CHECKLIST
- 1Affected ENG MAN START pbOFF
- 2Affected ENG MASTEROFF
- 3If APU BLEED available, APU BLEEDON
- 4If APU BLEED not available, X BLEED (opposite engine operating) - OPEN
- 5ENG MODE SelectorCRANK
- 6Affected ENG MAN START pbON
- 1PARK BRKON
- 2ATCNOTIFY
- 3If MAN CAB PR is in use, MAN V/S CTLFULL UP
- 4ENG MASTER 1 and 2OFF
- 5FIRE pbs (ENG and APU)PUSH
- 6AGENTs (ENG and APU), if requiredDISCH
- 7PA - THIS IS THE CAPTAIN. EVACUATE. EVACUATE. EVACUATE.
- 8EVAC COMMAND, if installedON
- 1APU, if availableENSURE STARTED
- 2APU bleed with ENG 1 FIRE pb pushedDO NOT USE
- 3APU bleed with ENG 2 FIRE pb pushedDO NOT USE UNLESS X BLEED SHUT
- 4APU bleed if wing anti-ice is requiredDO NOT USE
- 5Landing configurationCONF 3 PREFERRED
- 6Single engine autoland (A320)CONF FULL REQUIRED
- 7Autopilot on non-ILS approach in FINAL APP, NAV/VS or NAV/FPA - NOT ALLOWED
- 8Reverse thrust with one reverserBOTH THRUST LEVERS TO FULL REVERSE
- 9Fuel balanceMONITOR
- 1Limits - N1 ABOVE 100%, N2 ABOVE 100%, OR EGT ABOVE 635 degC
- 2THR LEVER of affected engineBELOW LIMIT
- 3Max value observed and time above limitsREPORT IN MAINTENANCE LOG
- 4If unable to maintain within limitsSHUT DOWN AFFECTED ENGINE
- 5If N1 at or above 109.4% or N2 at or above 105.7%, THR LEVERIDLE
- 6ENG MASTER of affected engineOFF
- 7ENG 1 (2) SHUT DOWN procedureAPPLY
- 1N2 vibration above 6.5 units during ground startABORT START
- 2Subsequent startAFTER COMPLETE SPOOL DOWN, MAX 3 ATTEMPTS
- 3If no icing conditions, ENG PARAMETERSCHECK
- 4If rapid increase above the advisory, THRUST LEVER of affected engine - RETARD
- 5If icing conditions, A/THROFF
- 6ENGINE ANTI ICECHECK, ON AT IDLE FAN SPEED ONE ENGINE AT A TIME
- 7THRUST LEVER, one engine at a timeINCREASE THRUST
- 1ConditionFADEC REVERTED TO N1 BACK-UP MODE, A/THR LOST
- 2ENG 1 N1 MODEON
- 3ENG 2 N1 MODEON
- 4N1 LIMITDO NOT EXCEED
- 5MAN THRADJUST
- 6Recovery of EPR mode - MAY BE ATTEMPTED BY SWITCHING OFF BOTH ENG N1 MODE pb-sw
FLIGHT2.22.0Checklist
Fenix A320 (CEO)MSFS 2024 · Emergency Procedures · 7procedures · 50 steps
ENG (1 or 2) Fire - On Ground7 steps
| 01 | THR LEVERSIDLE | |
| 02 | After aircraft is stopped, PARK BRKON | |
| 03 | Affected ENG MASTEROFF | |
| 04 | Affected ENG FIRE pbPUSH | |
| 05 | AGENT 1 and 2DISCH | |
| 06 | Condition of affected engineASSESS | |
| 07 | If requiredACCOMPLISH EVACUATION CHECKLIST |
Engine Tailpipe Fire6 steps
| 01 | Affected ENG MAN START pbOFF | |
| 02 | Affected ENG MASTEROFF | |
| 03 | If APU BLEED available, APU BLEEDON | |
| 04 | If APU BLEED not available, X BLEED (opposite engine operating) - OPEN | |
| 05 | ENG MODE SelectorCRANK | |
| 06 | Affected ENG MAN START pbON |
Evacuation8 steps
| 01 | PARK BRKON | |
| 02 | ATCNOTIFY | |
| 03 | If MAN CAB PR is in use, MAN V/S CTLFULL UP | |
| 04 | ENG MASTER 1 and 2OFF | |
| 05 | FIRE pbs (ENG and APU)PUSH | |
| 06 | AGENTs (ENG and APU), if requiredDISCH | |
| 07 | PA - THIS IS THE CAPTAIN. EVACUATE. EVACUATE. EVACUATE. | |
| 08 | EVAC COMMAND, if installedON |
After Engine Shutdown9 steps
| 01 | APU, if availableENSURE STARTED | |
| 02 | APU bleed with ENG 1 FIRE pb pushedDO NOT USE | |
| 03 | APU bleed with ENG 2 FIRE pb pushedDO NOT USE UNLESS X BLEED SHUT | |
| 04 | APU bleed if wing anti-ice is requiredDO NOT USE | |
| 05 | Landing configurationCONF 3 PREFERRED | |
| 06 | Single engine autoland (A320)CONF FULL REQUIRED | |
| 07 | Autopilot on non-ILS approach in FINAL APP, NAV/VS or NAV/FPA - NOT ALLOWED | |
| 08 | Reverse thrust with one reverserBOTH THRUST LEVERS TO FULL REVERSE | |
| 09 | Fuel balanceMONITOR |
ENG (1 or 2) N1 / N2 / EGT Overlimit7 steps
| 01 | Limits - N1 ABOVE 100%, N2 ABOVE 100%, OR EGT ABOVE 635 degC | |
| 02 | THR LEVER of affected engineBELOW LIMIT | |
| 03 | Max value observed and time above limitsREPORT IN MAINTENANCE LOG | |
| 04 | If unable to maintain within limitsSHUT DOWN AFFECTED ENGINE | |
| 05 | If N1 at or above 109.4% or N2 at or above 105.7%, THR LEVERIDLE | |
| 06 | ENG MASTER of affected engineOFF | |
| 07 | ENG 1 (2) SHUT DOWN procedureAPPLY |
High Engine Vibration7 steps
| 01 | N2 vibration above 6.5 units during ground startABORT START | |
| 02 | Subsequent startAFTER COMPLETE SPOOL DOWN, MAX 3 ATTEMPTS | |
| 03 | If no icing conditions, ENG PARAMETERSCHECK | |
| 04 | If rapid increase above the advisory, THRUST LEVER of affected engine - RETARD | |
| 05 | If icing conditions, A/THROFF | |
| 06 | ENGINE ANTI ICECHECK, ON AT IDLE FAN SPEED ONE ENGINE AT A TIME | |
| 07 | THRUST LEVER, one engine at a timeINCREASE THRUST |
ENG (1 or 2) EPR Mode Fault6 steps
| 01 | ConditionFADEC REVERTED TO N1 BACK-UP MODE, A/THR LOST | |
| 02 | ENG 1 N1 MODEON | |
| 03 | ENG 2 N1 MODEON | |
| 04 | N1 LIMITDO NOT EXCEED | |
| 05 | MAN THRADJUST | |
| 06 | Recovery of EPR mode - MAY BE ATTEMPTED BY SWITCHING OFF BOTH ENG N1 MODE pb-sw |